Kit Information - Front Spar Carry Thru Structure Reinforcement
Contains:
- Copy of Drawing (Qty 1) - 36-4004
- Installation Instructions (Qty 1) - 36-4005
- Doubler (Qty 1) - 36-430056-7
- Doubler (Qty 1) - 36-430056-8
- Shim (Qty 2) - 36-430056-9
- Angle (Qty 2) - 002-430013-27
- Bolt (Qty 8) - NAS2903-9
- Bolt (Qty 10) - NAS2904-10
- Pin (Qty 14) - 36-420016-1
- Nut (Qty 8) - MS21042L3
- Nut (Qty 10) - MS21042L4
- Rivet (Qty 20) - CR3243 4-3
- Rivet (Qty 2) - MS20470AD4-5
- Rivet (Qty 8) - MS20470AD4-6
- Rivet (Qty 8) - CR3243-5-5
- Rivet (Qty 2) - CR3243-4-4
- Rivet (Qty 2) - CR3213-4-2
- Scrim Cloth (24"" x 24"" Sheet) - AF3306
- Washer (Qty 8) - AN960-10
- Washer (Qty 10) - AN960-416
- Rivet (Qty 14) - CR3213-4-5
- Cutter (Qty 1) - BC10x3/32
- Cutter (Qty 1) - BC1/4x3/32
- Shaft (Qty 4) - BCP 3/32x6
- Rivet (Qty 2) - CR3243-4-2
- Rivet (Qty 10) - CR3243-4-1
- Collar (Qty 14) - HL94W-8
Required, Not Furnished with Kit:
- Adhesive (As Required) - EC 2216 B/A
- Degreasing Solvent (As Required)
- Corrosion Preventive Compound (As Required) - MIL-C-16173 Grade 2
- Adhesive (As Required) - EA9309NA
- Corrosion Proofing (As Required) - Alodine 1200
This kit provides parts and information necessary to install reinforcement parts on rear frame only on front spar carry thru structure on the following in-service aircraft:
- Model A36 Serials E356, E380, and After
- Model A36TC Serials EA1 thru EA241, EA243 thru EA272
- Model V35B Serials D9379, D9415 thru D10403
- Model F33A Serials CE401 and After
- Model F33C Serials CJ-31 thru CJ-179